Device for cooling a supporting structure of a heat shield, and heat shield
09702560 · 2017-07-11
Assignee
Inventors
Cpc classification
F23M2900/05002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R3/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R3/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R3/007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23M5/085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R3/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F23R3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R3/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23M5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A device (20, 29, 48, 64) for cooling a supporting structure of a heat shield (33, 60) to avoid scaling of the supporting structure due to the intake of hot gas. The device has a longitudinal axis (21) and a cooling air duct (22). The device is on the supporting structure with the longitudinal axis (21) intersecting the surface (51) of the supporting structure (34). In this position, the cooling air duct (22) extends from a device end (23) pointing towards the supporting structure. The device has at least one outlet duct downstream in the cooling air duct. The duct emerges out of the device (20, 29, 48, 64) laterally with respect to the longitudinal axis (21). The cooling air duct (22) corresponds to at least one cooling air passage (50) in the supporting structure (34).
Claims
1. A heat shield cooling device for a combustion chamber of a gas turbine, the cooling device comprising: a supporting structure, a plurality of heat shield tiles, tile holders releasably attaching the plurality of heat shield tiles to the supporting structure; each heat shield tile of the plurality of heat shield tiles has a cold side oriented towards the supporting structure and an opposite hot side which is exposed to a hot medium; each tile holder has a holding section for attaching to a heat shield tile of the plurality of heat shield tiles and an attachment section attached to the supporting structure for protecting the supporting structure from effects of hot gases; at least one cooling air passage arranged in the supporting structure; a post with a longitudinal axis and a cooling air duct extending through the post, the post is arranged on at least one of the at least one cooling air passage and the at least one of the at least one cooling air passage communicates cooling air into the cooling air duct for cooling the supporting structure; the post is on the supporting structure and is above a surface of the supporting structure, the cooling air duct extends through the post from the at least one of the at least one cooling air passage, downstream to at least one outlet duct that exits the post laterally with respect to the longitudinal axis; and the post on the supporting structure is located beneath a heat shield tile of the plurality of heat shield tiles, such that the at least one outlet duct of the post opens into an interspace between the cold side of the heat shield tile of the plurality of heat shield tiles and the supporting structure wherein the attachment section extends from the surface of the supporting structure at the post along a direction within the interspace, and the direction comprises a direction component parallel to the surface of the supporting structure.
2. The heat shield cooling device as claimed in claim 1, wherein the at least one outlet duct runs radially with respect to the longitudinal axis.
3. The heat shield cooling device as claimed in claim 1, further comprising at least two oppositely directed ones of the at least one outlet ducts.
4. The heat shield cooling device as claimed in claim 2, wherein the post has four of the at least one outlet ducts.
5. The heat shield cooling device as claimed in claim 1, further comprising: attachment slots running in the supporting structure, the attachment sections of the tile holders are releasably attached in the attachment slots; and the at least one cooling air passage opens into a bottom of the attachment slot, and the post is arranged in the bottom of the attachment slot at the at least one cooling air passage.
6. The heat shield cooling device as claimed in claim 5, further comprising the post is between two of the attachment sections of the tile holders.
7. The heat shield as claimed in claim 5, further comprising a cooling air slot in the bottom of the attachment slot, the post is sunk into the at least one of the at least one cooling air passage at least at the level of the bottom of the attachment slot, and the at least one outlet ducts of the post open into the cooling air slot.
8. The heat shield cooling device as claimed in claim 7, further comprising the cooling air slot comprises a runout at each ends of the cooling air slot.
9. The heat shield cooling device as claimed in claim 1, further comprising the supporting structure and the post are aligned such that the post is sunk into the supporting structure for enabling installing and removing of the plurality of heat shield tiles without interference from the post.
10. A combustion chamber which is clad with a heat shield, wherein the heat shield cooling device is as claimed in claim 1.
11. A gas turbine with at least one combustion chamber, wherein the at least one combustion chamber is as claimed in claim 10.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In the figures:
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DESCRIPTION OF EMBODIMENTS
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(11) The combustion system 9 communicates with for example an annular hot gas duct. There, multiple series-connected turbine stages form the turbine 14. Each turbine stage is formed from blade rings. As seen in the flow direction of a working medium, in the hot duct a row formed of stator vanes 17 alternates with a row formed of rotor blades 18. The stator vanes 17 are attached to an internal casing of a stator 19, whereas the rotor blades 18 of a row are attached to the rotor 3 by means of a turbine disk for example. Coupled to the rotor 3 is for example a generator (not shown).
(12) When the gas turbine is in operation, air is drawn in by the compressor 8 through the intake casing 6 and compressed. The compressed air which is made available at the turbine-side end of the compressor 8 is directed to the combustion system 9 and there it is mixed with fuel in the region of the combustion arrangement 11. The mixture is then combusted in the combustion system 9, with the aid of the combustion arrangement 11, forming a working gas flow. Thence, the working gas flow flows along the hot gas duct past the stator vanes 17 and the rotor blades 18. On the rotor blades 18, the working gas flow expands, transmitting an impulse so that the rotor blades 18 drive the rotor 3 and this drives the generator (not shown) which is coupled to the latter.
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(17) To provide protection from hot gases, a device 48 according to the invention for cooling the supporting structure 34 is arranged on the supporting structure 34 beneath the heat shield tile. According to the represented exemplary embodiment, the device 48 according to the invention is a post, set screw or cooling grub with a longitudinal axis 21 and a cooling air duct 22. The device 48 can thus also be termed a cooling grub 48. The post, set screw or cooling grub 48 is arranged on the supporting structure with its longitudinal axis 21 perpendicular to the surface 51 of the supporting structure, wherein the post cooling grub 48 is screwed into a cooling air passage 50 of the supporting structure with an end 23 oriented towards the supporting structure. The cooling air passage 50 is embodied as a cooling air bore. The cooling air duct 22 extends from the screwed-in end 23 and comprises, downstream, two outlet ducts 52a, 52b which exit the cooling grub 48 laterally with respect to the longitudinal axis 21. The cooling air bore 50 and the cooling air duct 22 line up with each other so that cooling air flowing out of the cooling air bore enters the cooling air duct 22 and, by means of the cooling grub 48, flows in the directions 53a, 53b into the interspace 46. The cooling air is thus introduced beneath the heat shield tile 35 far from the expansion gaps. This permits particularly effective cooling of the supporting structure. In addition, according to the invention, impingement cooling of the heat shield tile 35 is avoided. Since the post, set screw or cooling grub 48 in the represented exemplary embodiment is arranged between two attachment sections 40, 41 of the tile holders 38, 39, centrally beneath the heat shield tile 35, in particular those regions of the supporting structure to which the tile holders are attached are cooled. It is also possible for the length of the cooling air bore 50 to be chosen such that the cooling grub 48 can be entirely sunk into the former during installation and removal of the heat shield tiles.
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